EP3392600B1 - Dual-hardness clad steel plate and production method thereof - Google Patents

Dual-hardness clad steel plate and production method thereof Download PDF

Info

Publication number
EP3392600B1
EP3392600B1 EP16874827.5A EP16874827A EP3392600B1 EP 3392600 B1 EP3392600 B1 EP 3392600B1 EP 16874827 A EP16874827 A EP 16874827A EP 3392600 B1 EP3392600 B1 EP 3392600B1
Authority
EP
European Patent Office
Prior art keywords
hardness
steel plate
dual
hardness layer
layer
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
EP16874827.5A
Other languages
German (de)
English (en)
French (fr)
Other versions
EP3392600A4 (en
EP3392600A1 (en
Inventor
Xiaoting Zhao
Bo Yan
Liandeng Yao
Sihai JIAO
Hongbin Li
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Baoshan Iron and Steel Co Ltd
Original Assignee
Baoshan Iron and Steel Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Baoshan Iron and Steel Co Ltd filed Critical Baoshan Iron and Steel Co Ltd
Publication of EP3392600A1 publication Critical patent/EP3392600A1/en
Publication of EP3392600A4 publication Critical patent/EP3392600A4/en
Application granted granted Critical
Publication of EP3392600B1 publication Critical patent/EP3392600B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D9/00Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
    • C21D9/50Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for welded joints
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21BROLLING OF METAL
    • B21B1/00Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations
    • B21B1/38Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations for rolling sheets of limited length, e.g. folded sheets, superimposed sheets, pack rolling
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21BROLLING OF METAL
    • B21B37/00Control devices or methods specially adapted for metal-rolling mills or the work produced thereby
    • B21B37/74Temperature control, e.g. by cooling or heating the rolls or the product
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00Layered products comprising a layer of metal
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00Layered products comprising a layer of metal
    • B32B15/01Layered products comprising a layer of metal all layers being exclusively metallic
    • B32B15/011Layered products comprising a layer of metal all layers being exclusively metallic all layers being formed of iron alloys or steels
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D1/00General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
    • C21D1/18Hardening; Quenching with or without subsequent tempering
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D6/00Heat treatment of ferrous alloys
    • C21D6/004Heat treatment of ferrous alloys containing Cr and Ni
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D6/00Heat treatment of ferrous alloys
    • C21D6/005Heat treatment of ferrous alloys containing Mn
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D6/00Heat treatment of ferrous alloys
    • C21D6/008Heat treatment of ferrous alloys containing Si
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D8/00Modifying the physical properties by deformation combined with, or followed by, heat treatment
    • C21D8/02Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/0205Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips of ferrous alloys
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D8/00Modifying the physical properties by deformation combined with, or followed by, heat treatment
    • C21D8/02Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/0221Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
    • C21D8/0226Hot rolling
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D8/00Modifying the physical properties by deformation combined with, or followed by, heat treatment
    • C21D8/02Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/0247Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D8/00Modifying the physical properties by deformation combined with, or followed by, heat treatment
    • C21D8/02Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/0247Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
    • C21D8/0263Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment following hot rolling
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D8/00Modifying the physical properties by deformation combined with, or followed by, heat treatment
    • C21D8/02Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/04Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing
    • C21D8/0421Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing characterised by the working steps
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D8/00Modifying the physical properties by deformation combined with, or followed by, heat treatment
    • C21D8/02Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/04Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing
    • C21D8/0421Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing characterised by the working steps
    • C21D8/0426Hot rolling
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D8/00Modifying the physical properties by deformation combined with, or followed by, heat treatment
    • C21D8/02Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/04Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing
    • C21D8/0447Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing characterised by the heat treatment
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D8/00Modifying the physical properties by deformation combined with, or followed by, heat treatment
    • C21D8/02Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/04Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing
    • C21D8/0447Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing characterised by the heat treatment
    • C21D8/0463Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing characterised by the heat treatment following hot rolling
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D9/00Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
    • C21D9/42Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for armour plate
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D9/00Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
    • C21D9/46Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D9/00Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
    • C21D9/46Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals
    • C21D9/48Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals deep-drawing sheets
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/02Ferrous alloys, e.g. steel alloys containing silicon
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/04Ferrous alloys, e.g. steel alloys containing manganese
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/06Ferrous alloys, e.g. steel alloys containing aluminium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/08Ferrous alloys, e.g. steel alloys containing nickel
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/12Ferrous alloys, e.g. steel alloys containing tungsten, tantalum, molybdenum, vanadium, or niobium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/14Ferrous alloys, e.g. steel alloys containing titanium or zirconium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/16Ferrous alloys, e.g. steel alloys containing copper
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/32Ferrous alloys, e.g. steel alloys containing chromium with boron
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/42Ferrous alloys, e.g. steel alloys containing chromium with nickel with copper
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/44Ferrous alloys, e.g. steel alloys containing chromium with nickel with molybdenum or tungsten
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/50Ferrous alloys, e.g. steel alloys containing chromium with nickel with titanium or zirconium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/54Ferrous alloys, e.g. steel alloys containing chromium with nickel with boron
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21BROLLING OF METAL
    • B21B1/00Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations
    • B21B1/38Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations for rolling sheets of limited length, e.g. folded sheets, superimposed sheets, pack rolling
    • B21B2001/383Cladded or coated products
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21BROLLING OF METAL
    • B21B1/00Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations
    • B21B1/38Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations for rolling sheets of limited length, e.g. folded sheets, superimposed sheets, pack rolling
    • B21B2001/386Plates
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/50Properties of the layers or laminate having particular mechanical properties
    • B32B2307/536Hardness
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D2211/00Microstructure comprising significant phases
    • C21D2211/001Austenite
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D2211/00Microstructure comprising significant phases
    • C21D2211/008Martensite
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D2251/00Treating composite or clad material
    • C21D2251/02Clad material
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41HARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H5/00Armour; Armour plates
    • F41H5/02Plate construction
    • F41H5/04Plate construction composed of more than one layer
    • F41H5/0442Layered armour containing metal
    • F41H5/045Layered armour containing metal all the layers being metal layers

Definitions

  • the present disclosure relates to a steel plate and a method of manufacturing the same, particularly to a clad steel plate and a method of manufacturing the same.
  • a bullet-proof armour is disposed on an exterior side of the cabinet body, wherein the bullet-proof armour is formed by bonding a 616 armour steel plate to a Kevlar composite plate, wherein the 616 armour steel plate is an outer layer of the bullet-proof armour, and the Kevlar composite plate is the inner layer of the bullet-proof armour.
  • An 8 mm thick steel plate is used for the 616 armour steel plate of the outer layer, and a 7mm thick steel plate is used for the Kevlar composite plate of the inner layer.
  • this Chinese patent literature is silent on characteristics or comprehensive performances of related steel plate products.
  • EP 2 123 447 A1 teaches a bonding material having a first alloy steel layer and a second alloy steel layer of different alloy steels.
  • the first layer is of the following alloy composition (wt.%): C 0.06-1.05; Si 0.05-1.65; Mn 0.3-1.55; Cr not more than 1.2%; Ti not more than 0.13%; Mo not more than 0.7%; Nb not more than 0.1%; B not more than 0.005%; P not more than 0.08%; S not more than 0.01%; Ni not more than 4%; V not more than 0.5%; and the rest Fe and unavoidable impurities.
  • CN 105 088 090 A discloses an armor plate with the tensile strength being 2000 MPa and the Brinell hardness being 600.
  • the armor plate comprises, by mass, 0.35%-0.45% of C, 0.80%-1.60% of Si, 0.3%-1.0% of Mn, 0.02%-0.06% of Al, 0.3%-1.2% of Ni, 0.30%-1.00% of Cr, 0.20%-0.80% of Mo, 0.20%-0.60% of Cu, 0.01%-0.05% of Ti, 0.001%-0.003% of B and the balance Fe and unavoidable impurities.
  • One object of the invention is to provide a dual-hardness clad steel plate with two different surfaces having two different hardness properties.
  • One surface of the dual-hardness clad steel plate has an ultra-high hardness, while another surface opposite to this surface has a relatively low hardness and a relatively high low-temperature toughness.
  • the dual-hardness clad steel plate according to this disclosure realizes a combination of high hardness, low hardness and high toughness.
  • the dual-hardness clad steel plate according to this disclosure exhibits superior machinability and excellent bullet-proof performance.
  • the present disclosure proposes a dual-hardness clad steel plate as defined in claim 1. Further improvements are subject to the dependent claims.
  • a low-hardness layer means it has a lower hardness in comparison with a high-hardness layer.
  • the low-hardness layer is Mn13 steel, its Brinell hardness is lower than 250.
  • the above high-hardness layer comprises the following chemical elements in mass percentage:
  • C It may have a function of solid solution strengthening in steel, and it's a strengthening element that makes the greatest contribution to steel strength at the lowest cost.
  • C It's desired to have a relatively high content of carbon in steel.
  • an unduly high carbon content will have a negative impact on weldability and toughness of steel.
  • the carbon content in the high-hardness layer of the dual-harness clad steel plate according to the disclosure is controlled in the range of 0.35-0.45%.
  • Si is an element for removing oxygen.
  • Si can dissolve in ferrite and has a function of solid solution strengthening. Silicon is only secondary to carbon, nitrogen, phosphorus and excels other alloy elements in this function. Therefore, Si can improve steel strength and hardness notably. If the solid solution strengthening function of Si is desired, the amount of Si to be added is generally not lower than 0.6%. In the above high-hardness layer, the Si content is controlled in the range of 0.8-1.6% to effect solid solution strengthening.
  • Mn can reduce a critical cooling rate of steel, thereby promoting hardenability greatly, and it may have a solid solution strengthening effect on steel.
  • an unduly high Mn content will result in a sharply decreased martensitic transformation temperature, leading to increased residual austenite at room temperature, which is undesirable for increasing steel strength.
  • coarse MnS will be generated in a center segregation area of a casting blank, reducing toughness of a plate at the middle of its thickness.
  • the Mn content in the above high-hardness layer is controlled in the range of 0.3-1.0%.
  • Al is also an element for removing oxygen. Meanwhile, Al can also form fine, insoluble AlN particles with nitrogen, thereby refining steel microstructure and inhibiting BN formation, so that B is still present in a solid solution state, which ensures steel hardenability. Nevertheless, once an Al content exceeds 0.06%, coarse alumina inclusions will form in steel. Therefore, the Al content in the high-hardness layer is controlled in the range of 0.02-0.06%.
  • Ni in steel only dissolves in matrix phase ferrite and austenite, and no carbide will form. It exhibits a strong effect in stabilizing austenite.
  • Ni is a main element for ensuring high steel toughness.
  • the Ni content in the high-hardness layer is set in the range of 0.3-1.2%.
  • Cr is an element for reducing an austenitic phase zone, and it's also a moderately strong carbide forming element. Cr is also soluble in ferrite. Cr can stabilize austenite, and shift a C curve to the right, thereby reducing a critical cooling rate, and thus improving steel hardenability.
  • the Cr content in the above high-hardness layer is controlled in the range of 0.3-1.0%.
  • Mo As Mo in steel can be present in a solid solution phase and a carbide phase at the same time, Mo exhibits both effects of solid solution strengthening and carbide dispersion strengthening for steel, thereby acting to improve steel hardness and strength remarkably. As such, the Mo content in the above high-hardness layer is controlled in the range of 0.20-0.80%.
  • Cu in steel is mainly present in a solid solution state and a precipitate state of elemental phase.
  • Solid-dissolved Cu may have a function of solid solution strengthening. Since the solid solubility of Cu in ferrite decreases rapidly as temperature decreases, oversaturated solid-dissolved Cu will precipitate in the form of elementary substance at low temperatures, thereby introducing an effect of precipitation strengthening. Addition of Cu to the above high-hardness layer in an amount of 0.20 - 0.60% can improve atmospheric corrosion resistance of steel significantly.
  • Ti can form titanium carbide, titanium nitride or titanium carbonitride with C, N in steel, and thus has an effect of refining austenite grains at a stage of heating and rolling a steel blank, thereby improving steel strength and toughness.
  • an unduly high Ti content will result in formation of a large amount of coarse titanium nitride in steel, having a negative impact on steel strength and toughness.
  • the Ti content in the above high-hardness layer is controlled in the range of 0.01-0.05%.
  • B Addition of B in a small amount can significantly improve steel hardenability, and allows for easy obtainment of a martensitic structure in steel. Nevertheless, it's undesirable to add too much B, because a relatively strong bonding force exits between B and a crystalline boundary, so that B tends to segregate at the crystalline boundary, thereby affecting the overall properties of the steel. As such, the B content in the above high-hardness layer is controlled in the range of 0.001-0.003%.
  • the main unavoidable impurities in the high-hardness layer of the dual-hardness clad steel plate according to the disclosure are P and S.
  • microstructure of the above high-hardness layer includes martensite and a small amount of residual austenite.
  • a proportion of the above residual austenitic phase is less than 1%.
  • the microstructure of the high-hardness layer is controlled to be martensite and a small amount of residual austenite for the following reasons: residual austenite is a structure that will occur unavoidably when over-cooled austenite undergoes phase change after quenching, and strict control over the residual austenite helps ensure the properties of a particular type of steel; while in martensite, due to the solid solution strengthening effect of the carbon dissolved in ⁇ phase and the strengthening effect caused by the presence of a substructure of high density dislocations, martensite is characterized by high hardness. Hence, to guarantee high hardness of the high-hardness layer, nearly all of the microstructure needs to be controlled to be a martensitic structure.
  • the above low-hardness layer comprises the following chemical elements in mass percentage:
  • Mo may be further added into the above low-hardness layer in an amount of 0.90-1.80%.
  • the reason for further adding alloy element Mo into the low-hardness layer is that Mo can bond relatively strongly with iron, and Mo will not spread easily due to a relatively large atomic size of molybdenum. Therefore, few carbides precipitate in as-cast high manganese steel into which Mo is added, and the carbides do not present a network distribution on austenite grain boundaries. After water toughening treatment, molybdenum is solid-dissolved in austenite, and thus delays decomposition of austenite, which is advantageous for strength and toughness of high manganese steel.
  • the dual-hardness clad steel plate according to the disclosure has an impact strength of no less than 50 J at -40°C.
  • the high-hardness layer and the low-hardness layer described above has a thickness ratio of (0.43-3): 1.
  • Another object of the disclosure is to provide a method of manufacturing a dual-hardness clad steel plate.
  • This manufacture method can afford a clad steel plate comprising two surfaces having different hardness features, wherein one of the surfaces has an ultra-high hardness, and the other surface has a relatively low hardness and a relatively high low-temperature toughness.
  • This manufacture method allows for a combination of high hardness, low hardness and high toughness in the same steel plate.
  • the dual-hardness clad steel plate obtained by this manufacture method exhibits superior machinability and excellent bullet-proof performance.
  • the method of manufacturing a dual-hardness clad steel plate according to the disclosure comprises the following steps:
  • One key point to the method of manufacturing a dual-hardness clad steel plate according to the disclosure is atomic bonding of slabs having different hardness features by clad rolling.
  • Another key point to the manufacture method is setting of the heating temperature in the heat treatment step to 1050-1100°C, so as to obtain a single homogeneous austenitic microstructure in the low-hardness layer slab. Cooling the heated clad plate with water having a temperature lower than 40°C is aimed to water toughen the low-hardness layer slab of the clad plate, so as to obtain a single austenitic microstructure.
  • this heat treatment step is equivalent to quenching treatment for the high-hardness layer slab of the clad plate, so as to obtain a martensitic microstructure.
  • a heating temperature is 1130-1250°C, and a heating time is 120-180min.
  • step (3) control of the heating temperature in the range of 1130-1250°C and the heating time in the range of 120-180min is aimed to ensure that each of the assembled slabs should have a homogeneous alloy composition, so as to obtain a complete austenitic phase in the low-hardness layer, thereby reducing a yield stress of the slab, and thus reducing deformation resistance of a final clad steel plate.
  • a finishing rolling temperature is controlled in the range of 850-1000 °C.
  • step (4) setting of the finishing rolling temperature to ⁇ 950 °C is also aimed to reduce the deformation resistance of the composite slab in the rolling stage.
  • the alloy ingredients in the technical solution of the disclosure are simple and readily controllable.
  • the main ingredients include a medium content of carbon and low contents of alloying elements.
  • Full advantage is taken of the solid solution strengthening effect of the alloy elements including C, Si, Mn, Cr, Ni, Cu, B and the like, as well as the function of the fine Ti(C, N) particles formed from the micro-alloying element Ti and elements C, N in refining austenitic grains.
  • a dual-hardness clad steel plate having different hardness features is obtained by process steps of rolling, heat treatment, etc.
  • microstructure of the high-hardness layer in the dual-hardness clad steel plate according to the disclosure is martensite and a small amount of residual austenite, while the microstructure of the low-hardness layer in the dual-hardness clad steel plate according to the disclosure is purely austenite.
  • a thickness ratio of the high-hardness layer to the low-hardness layer may be regulated in light of the circumstances in practical production. Thereafter, slabs may be assembled to produce a dual-hardness clad steel plate having a high hardness and a low hardness at the same time.
  • water toughening treatment of the low-hardness layer in the clad steel plate and quenching treatment of the high-hardness layer in the clad steel plate are fulfilled in the same process step of heat treatment.
  • the dual-hardness clad steel plate according to the disclosure has different surface hardnesses, wherein one surface has a Brinell hardness > 600, and another surface has a Brinell hardness ⁇ 250.
  • the dual-hardness clad steel plate exhibits excellent bullet-proof performance, and it's able to meet the bullet-proof requirement imposed on steel plates by domestic armored vehicles.
  • the dual-hardness clad steel plate according to the disclosure has excellent low-temperature toughness, wherein its Charpy V longitudinal impact strength at -40 °C is not lower than 50 J.
  • the dual-hardness clad steel plate according to the disclosure also has good machinability, suitable for manufacture of bullet-proof vehicles and structural components thereof.
  • the method of manufacturing a dual-hardness clad steel plate according to the disclosure can provide a clad steel plate having different surface hardness features, and this steel plate exhibits excellent low-temperature toughness, superior bullet-proof performance and good machinability.
  • the method of manufacturing a dual-hardness clad steel plate according to the disclosure is simple and easy to practice, suitable for steady production on production lines for medium- and large-thickness plates.
  • Table 1 lists the mass percentages of the various chemical elements in the high-hardness layers and low-hardness layers of the dual-hardness clad steel plates in Examples A1-A6.
  • Table 1 (wt%, the balance is Fe and other unavoidable impurities)
  • Table 2 lists the specific process parameters in the manufacture method for the dual-hardness clad steel plates in Examples A1-A6.
  • the dual-hardness clad steel plates in the above Examples were sampled for various mechanical properties tests.
  • the relevant mechanical properties obtained in the tests are listed in Table 3.
  • the samples of the dual-hardness clad steel plates were subjected to shooting tests.
  • the results of the tests are listed in Table 4.
  • Table 3 lists the parameters of the relevant mechanical properties of the dual-hardness clad steel plates in Examples A1-A4.
  • Table 3 No. Brinell hardness of high-hardness layer (HB10/3000) Brinell hardness of low-hardness layer (HB10/3000) Impact strength of clad steel plate KV2(-40°C)/J A1 613 217 60 A2 618 230 54 A3 620 210 90 A4 630 210 210 A5 620 223 80 A6 615 235 190 Note: The impact samples for test plates in A1 and A2 had a size of 5 ⁇ 10 ⁇ 55mm; and the impact samples for test plates in A3-A6 had a size of 10 ⁇ 10 ⁇ 55mm.
  • HB10/3000 represents a Brinell hardness value measured under a 3000 kg load using an indenter of 10 mm in diameter.
  • each of the high-hardness layers of the dual-hardness clad steel plates in Examples A1-A6 has a Brinell hardness ⁇ 613HB; and each of the low-hardness layers has a Brinell hardness ⁇ 250HB.
  • each of the dual-hardness clad steel plates in Examples A1-A6 has an impact strength KV2 (-40°C)>50J. This indicates that the clad steel plates in the above examples have good low-temperature toughness.
  • Table 4 lists the shooting test results of the dual-hardness clad steel plates in Examples A1-A4.
  • Table 4 No. Bullet type Shooting distance (m) Shooting velocity (m/s) Result A1 M16 automatic rifle, 5.56 ⁇ 45 30 981/985/983 Not shot through A2 M16 automatic rifle, 5.56 ⁇ 45 30 986/986/985 Not shot through A3 M16 automatic rifle, 5.56 ⁇ 45 10 984/985/983 Not shot through A4 M16 automation rifle, 5.56 ⁇ 45 10 986/984/987 Not shot through A5 M16 automatic rifle, 5.56 ⁇ 45 10 976/981/982 Not shot through A6 M16 automatic rifle, 10 971/975/973 Not shot 5.56 ⁇ 45 through
  • Fig. 1 shows a metallographic structure of the dual-hardness clad steel plate according to Example A4.
  • Fig. 2 shows a microstructure of the high-hardness layer in the dual-hardness clad steel plate according to Example A4.
  • this dual-hardness clad steel plate has a high-hardness layer and a low-hardness layer, wherein the upper layer is the high-hardness layer whose microstructure is martensite and a small amount of residual austenite; wherein the lower layer is the low-hardness layer whose microstructure is purely austenite.
  • Fig. 2 nearly all of the microstructure of the high-hardness layer is martensite, with a proportion of the residual austenitic phase being lower than 1%.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Ceramic Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Heat Treatment Of Steel (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Laminated Bodies (AREA)
  • Heat Treatment Of Articles (AREA)
EP16874827.5A 2015-12-14 2016-12-14 Dual-hardness clad steel plate and production method thereof Active EP3392600B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN201510926272.9A CN105499269A (zh) 2015-12-14 2015-12-14 一种双重硬度复合钢板及其制造方法
PCT/CN2016/109781 WO2017101770A1 (zh) 2015-12-14 2016-12-14 一种双重硬度复合钢板及其制造方法

Publications (3)

Publication Number Publication Date
EP3392600A1 EP3392600A1 (en) 2018-10-24
EP3392600A4 EP3392600A4 (en) 2019-05-15
EP3392600B1 true EP3392600B1 (en) 2021-03-24

Family

ID=55707789

Family Applications (1)

Application Number Title Priority Date Filing Date
EP16874827.5A Active EP3392600B1 (en) 2015-12-14 2016-12-14 Dual-hardness clad steel plate and production method thereof

Country Status (6)

Country Link
US (1) US10851435B2 (zh)
EP (1) EP3392600B1 (zh)
JP (1) JP6644163B2 (zh)
KR (1) KR102138313B1 (zh)
CN (1) CN105499269A (zh)
WO (1) WO2017101770A1 (zh)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105499269A (zh) * 2015-12-14 2016-04-20 宝山钢铁股份有限公司 一种双重硬度复合钢板及其制造方法
CN107310218B (zh) * 2016-04-26 2019-03-29 宝山钢铁股份有限公司 一种复合防弹钢板及其制造方法
CN107310219B (zh) 2016-04-26 2019-03-29 宝山钢铁股份有限公司 一种冷弯加工性能优良的防弹钢板及其制造方法
CN109835014B (zh) * 2017-11-28 2021-03-12 宝山钢铁股份有限公司 一种高强高韧耐磨复合钢板及其制造方法
CN109835015B (zh) * 2017-11-28 2021-03-12 宝山钢铁股份有限公司 一种耐磨复合钢板及其制造方法
CN109835013B (zh) * 2017-11-28 2021-03-12 宝山钢铁股份有限公司 一种高强耐磨复合钢板及其制造方法
JP7070794B2 (ja) * 2019-03-29 2022-05-18 日本製鉄株式会社 高強度熱間圧延鋼板
DE102019116363A1 (de) 2019-06-17 2020-12-17 Benteler Automobiltechnik Gmbh Verfahren zur Herstellung eines Panzerungsbauteils für Kraftfahrzeuge
CN112756408A (zh) * 2020-12-21 2021-05-07 山东荣升重型机械股份有限公司 多个工件合轧方法
WO2022183736A1 (zh) * 2021-03-05 2022-09-09 江苏康瑞新材料科技股份有限公司 一种手机边框及制造方法
EP4302893A1 (en) * 2021-03-05 2024-01-10 Jiangsu Kangrui New Material Technology Co., Ltd. Combined machining method for metal material
CN113106351A (zh) * 2021-04-20 2021-07-13 吉安锐迈管道配件有限公司 一种超低温9Ni钢及其制备工艺
CN113528949A (zh) * 2021-06-22 2021-10-22 河钢股份有限公司承德分公司 一种550MPa级太阳能支架用热轧钢卷及其生产方法
CN113399948A (zh) * 2021-07-02 2021-09-17 东北大学 一种生产厚度100mm以上规格1000MPa水电钢的方法
CN114891989B (zh) * 2022-06-20 2023-05-02 河北普阳钢铁有限公司 一种耐磨耐蚀复合钢板的轧制工艺

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3694174A (en) 1971-05-13 1972-09-26 Us Army Dual property steel armor
AT372113B (de) * 1981-12-22 1983-09-12 Voest Alpine Ag Dreilagiger formkoerper, insbesondere blech, von hoher verschleissfestigkeit
JP3545963B2 (ja) * 1998-03-30 2004-07-21 株式会社神戸製鋼所 高靱性超耐摩耗鋳鋼及びその製造方法
CN2715093Y (zh) * 2004-08-24 2005-08-03 天津市圣恺工业技术发展有限公司 用于坦克的外挂式复合装甲板
CN100371121C (zh) * 2005-04-06 2008-02-27 吉欣(英德)热轧不锈复合钢有限公司 一种压制钎焊热轧复合坯的加工方法
CN101214497A (zh) * 2008-01-07 2008-07-09 吉欣(英德)热轧不锈复合钢有限公司 采用复合坯同时轧制三块金属复合板的方法
CN101215669B (zh) * 2008-01-08 2011-07-06 济南钢铁股份有限公司 一种大型石油储罐用高强度厚钢板及其低成本制造方法
PL2123447T3 (pl) * 2008-05-07 2019-05-31 Thyssenkrupp Steel Europe Ag Tworzywo kompozytowe z efektem ochrony balistycznej
US8176831B2 (en) 2009-04-10 2012-05-15 Nova Research, Inc. Armor plate
JP2010280127A (ja) * 2009-06-04 2010-12-16 Nippon Steel Corp 張り剛性に優れた複合パネル
CN101892443A (zh) * 2010-07-09 2010-11-24 天津钢管集团股份有限公司 屈服强度170~180ksi钢级的高强高韧性石油套管及其制造方法
US20120156085A1 (en) * 2010-12-14 2012-06-21 Thompson Peter T Blast Resistant, Non-Magnetic, Stainless Steel Armor
US9182196B2 (en) * 2011-01-07 2015-11-10 Ati Properties, Inc. Dual hardness steel article
CN202750372U (zh) 2012-09-17 2013-02-20 南京恩瑞特实业有限公司 一种新型防弹机柜
CN103451546B (zh) 2012-12-24 2016-06-15 河南理工大学 一种高耐磨高锰钢及其制备方法
CN103484599B (zh) * 2013-08-20 2015-05-20 山西太钢不锈钢股份有限公司 一种高锰耐磨钢的冶炼方法
CN104501660A (zh) * 2015-01-04 2015-04-08 成都索伊新材料有限公司 一种装甲车用轻质复合防弹结构
CN105088090A (zh) * 2015-08-28 2015-11-25 宝山钢铁股份有限公司 一种抗拉强度2000MPa级的防弹钢板及其制造方法
CN105499269A (zh) * 2015-12-14 2016-04-20 宝山钢铁股份有限公司 一种双重硬度复合钢板及其制造方法

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None *

Also Published As

Publication number Publication date
EP3392600A4 (en) 2019-05-15
JP2019505687A (ja) 2019-02-28
JP6644163B2 (ja) 2020-02-12
CN105499269A (zh) 2016-04-20
KR102138313B1 (ko) 2020-08-14
EP3392600A1 (en) 2018-10-24
US20180363093A1 (en) 2018-12-20
WO2017101770A1 (zh) 2017-06-22
US10851435B2 (en) 2020-12-01
KR20180097176A (ko) 2018-08-30

Similar Documents

Publication Publication Date Title
EP3392600B1 (en) Dual-hardness clad steel plate and production method thereof
KR102585250B1 (ko) 인장강도 2000MPa급 방탄강판 및 그의 제조방법
CN105543649B (zh) 一种三层复合钢板及其制造方法
KR102119959B1 (ko) 우수한 경도와 충격인성을 갖는 내마모강 및 그 제조방법
KR101490567B1 (ko) 용접성이 우수한 고망간 내마모강 및 그 제조방법
JP6743282B2 (ja) 複合防護用鋼板及びその製造方法
KR102314432B1 (ko) 저온 충격인성이 우수한 고경도 내마모강 및 이의 제조방법
WO2021241606A1 (ja) 耐摩耗鋼板および耐摩耗鋼板の製造方法
EP2799583A1 (en) Abrasion resistant steel with excellent toughness and weldability
KR101439629B1 (ko) 내마모성이 우수한 내마모용 강재 및 그 제조방법
JPH0615686B2 (ja) 耐摩毛構造用鋼材の製造法
WO2017186112A1 (zh) 一种冷弯加工性能优良的防护用钢板及其制造方法
KR102498144B1 (ko) 저온 충격인성이 우수한 고경도 방탄강 및 이의 제조방법
JP7063420B1 (ja) 耐摩耗鋼板および耐摩耗鋼板の製造方法
KR102498141B1 (ko) 저온 충격인성이 우수한 고경도 방탄강 및 이의 제조방법
KR102498147B1 (ko) 저온 충격인성이 우수한 고경도 방탄강 및 이의 제조방법
KR102498150B1 (ko) 저온 충격인성이 우수한 고경도 방탄강 및 이의 제조방법
KR102498142B1 (ko) 저온 충격인성이 우수한 고경도 방탄강 및 이의 제조방법
WO2017208329A1 (ja) 低温靭性に優れた高張力鋼板
KR102498149B1 (ko) 저온 충격인성이 우수한 고경도 방탄강 및 이의 제조방법
US20220154317A1 (en) Iron-based alloy composition, parts produced from this composition and production method
US20230203614A1 (en) Abrasion-resistant steel plate and method of producing abrasion-resistant steel plate
CN115478210A (zh) 一种1500MPa级高强度自强韧防护钢板及其制造方法
GB2602872A (en) Ultrahigh-strength reinforcing bar and manufacturing method therefor
KR101439628B1 (ko) 내마모용 강재 및 그 제조방법

Legal Events

Date Code Title Description
STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE

PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20180607

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

DAV Request for validation of the european patent (deleted)
DAX Request for extension of the european patent (deleted)
A4 Supplementary search report drawn up and despatched

Effective date: 20190417

RIC1 Information provided on ipc code assigned before grant

Ipc: C22C 38/44 20060101ALI20190411BHEP

Ipc: C21D 8/02 20060101ALI20190411BHEP

Ipc: C21D 9/42 20060101ALI20190411BHEP

Ipc: C22C 38/42 20060101ALI20190411BHEP

Ipc: B23K 20/04 20060101ALI20190411BHEP

Ipc: B32B 15/00 20060101ALI20190411BHEP

Ipc: C21D 1/18 20060101ALI20190411BHEP

Ipc: C21D 8/04 20060101ALI20190411BHEP

Ipc: C21D 6/00 20060101ALI20190411BHEP

Ipc: B32B 15/01 20060101ALI20190411BHEP

Ipc: C22C 38/04 20060101ALI20190411BHEP

Ipc: C22C 38/50 20060101ALI20190411BHEP

Ipc: C21D 9/50 20060101ALI20190411BHEP

Ipc: C22C 38/06 20060101ALI20190411BHEP

Ipc: C21D 9/46 20060101ALI20190411BHEP

Ipc: B21B 1/38 20060101ALI20190411BHEP

Ipc: C22C 38/02 20060101ALI20190411BHEP

Ipc: C22C 38/54 20060101ALI20190411BHEP

Ipc: C21D 9/48 20060101ALI20190411BHEP

Ipc: F41H 5/04 20060101AFI20190411BHEP

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: EXAMINATION IS IN PROGRESS

17Q First examination report despatched

Effective date: 20200406

REG Reference to a national code

Ref country code: DE

Ref legal event code: R079

Ref document number: 602016055015

Country of ref document: DE

Free format text: PREVIOUS MAIN CLASS: F41H0005040000

Ipc: C22C0038500000

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

RIC1 Information provided on ipc code assigned before grant

Ipc: C22C 38/44 20060101ALI20200928BHEP

Ipc: C21D 9/42 20060101ALI20200928BHEP

Ipc: C21D 8/02 20060101ALI20200928BHEP

Ipc: C21D 8/04 20060101ALI20200928BHEP

Ipc: F41H 5/04 20060101ALN20200928BHEP

Ipc: C22C 38/06 20060101ALI20200928BHEP

Ipc: C21D 9/50 20060101ALI20200928BHEP

Ipc: B23K 20/04 20060101ALI20200928BHEP

Ipc: C22C 38/54 20060101ALI20200928BHEP

Ipc: B32B 15/00 20060101ALI20200928BHEP

Ipc: C22C 38/02 20060101ALI20200928BHEP

Ipc: C22C 38/50 20060101AFI20200928BHEP

Ipc: C21D 9/46 20060101ALI20200928BHEP

Ipc: C22C 38/04 20060101ALI20200928BHEP

Ipc: C21D 1/18 20060101ALI20200928BHEP

Ipc: C21D 6/00 20060101ALI20200928BHEP

Ipc: C22C 38/42 20060101ALI20200928BHEP

Ipc: B21B 1/38 20060101ALN20200928BHEP

Ipc: B32B 15/01 20060101ALI20200928BHEP

RIC1 Information provided on ipc code assigned before grant

Ipc: C21D 8/02 20060101ALI20201006BHEP

Ipc: C21D 6/00 20060101ALI20201006BHEP

Ipc: C21D 1/18 20060101ALI20201006BHEP

Ipc: C22C 38/44 20060101ALI20201006BHEP

Ipc: C22C 38/50 20060101AFI20201006BHEP

Ipc: C21D 9/42 20060101ALI20201006BHEP

Ipc: C22C 38/02 20060101ALI20201006BHEP

Ipc: C22C 38/54 20060101ALI20201006BHEP

Ipc: C22C 38/04 20060101ALI20201006BHEP

Ipc: B32B 15/01 20060101ALI20201006BHEP

Ipc: C21D 9/50 20060101ALI20201006BHEP

Ipc: C22C 38/06 20060101ALI20201006BHEP

Ipc: C22C 38/42 20060101ALI20201006BHEP

Ipc: F41H 5/04 20060101ALN20201006BHEP

Ipc: B21B 1/38 20060101ALN20201006BHEP

Ipc: C21D 9/46 20060101ALI20201006BHEP

INTG Intention to grant announced

Effective date: 20201019

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

RIN1 Information on inventor provided before grant (corrected)

Inventor name: YAN, BO

Inventor name: YAO, LIANDENG

Inventor name: ZHAO, XIAOTING

Inventor name: JIAO, SIHAI

Inventor name: LI, HONGBIN

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 1374598

Country of ref document: AT

Kind code of ref document: T

Effective date: 20210415

Ref country code: DE

Ref legal event code: R096

Ref document number: 602016055015

Country of ref document: DE

REG Reference to a national code

Ref country code: FI

Ref legal event code: FGE

REG Reference to a national code

Ref country code: SE

Ref legal event code: TRGR

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG9D

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20210624

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20210324

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20210625

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20210624

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20210324

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20210324

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20210324

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 1374598

Country of ref document: AT

Kind code of ref document: T

Effective date: 20210324

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20210324

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20210324

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20210324

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20210324

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20210324

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20210324

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20210324

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20210324

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20210324

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20210726

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20210724

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602016055015

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20210324

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20210324

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20210324

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20210324

26N No opposition filed

Effective date: 20220104

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20210724

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20210324

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20211214

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20211231

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20211214

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20211214

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20211214

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20211231

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20211231

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20211231

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20210324

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20210324

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20161214

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: SE

Payment date: 20231218

Year of fee payment: 8

Ref country code: FR

Payment date: 20231123

Year of fee payment: 8

Ref country code: FI

Payment date: 20231124

Year of fee payment: 8

Ref country code: DE

Payment date: 20231206

Year of fee payment: 8

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20210324